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Based on the Joule heating effect of gas discharge in the working process of the plasma actuator, the plasma synthetic jet is simulated with a three-dimensional phenomenological model, under the assumption of local thermodynamic equilibrium plasma.The flow field evolution process of the plasma synthetic jet during a whole cycle is obtained. The results show that in the self-sustained periodical jet built by a single energy deposition, there is a maxium pulse frequency–saturated frequency which could relaize that the cavity is recovered sufficiently. Large energy deposition, small exit orifice diameter and high diameter-height ratio with the same cavity volume could induce higher speed jet, and the increase of the jet speed occurs concurrently with the decrease of the saturated frequency. During a saturated cycle, up to 16% of the mass in the cacity is expelled, but the recovery can only achieve about 90% of the initial mass in the cavity. Plasma synthetic jet actuator is supplied by a capacitive power supply at atmospheric pressure, the fractions of power that go into gas heating and jet kinetic energy are 5% and 1.6% respectively.
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Keywords:
- plasma actuator /
- synthetic jet /
- energy efficiency /
- saturation frequency
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[2] Leonov S, Yarantsev D 2008 J. Propul. Power 24 1168
[3] Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y 2009 J. Phys. D: Appl. Phys. 42 165503
[4] Grossman K R, Cybyk B Z, van Wie D M 2003 41st Aerospace Science Meeting and Exhibit Reno Nevada, USA, January 6-9, 2003
[5] Roth J 2003 Phys. Plasmas 42 165503
[6] Moreau E 2007 J. Phys. D: Appl. Phys. 40 605
[7] Zhang P F, Wang J J, Feng L H, Wang G B 2010 AIAA J. 48 249
[8] Li Y H, Wu Y, Liang H, Song H M, Jia M 2010 Chin. Sci. Bull. 55 3060 (in Chinese) [李应红, 吴云, 梁华, 宋慧敏, 贾敏 2010 科学通报 55 3060]
[9] Li G, Li Y M, Xu Y J, Zhang Y, Li H M, Nie C Q, Zhu J Q 2009 Acta Phys. Sin. 58 4026 (in Chinese) [李刚, 李轶明, 徐燕骥, 张翼, 李汉明, 聂超群, 朱俊强 2009 58 4026]
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[14] Ko H S, Haack S J, Land H B, Cybyk B, Katz J, Kim H J 2010 Flow Meas. Instrum. 21 443
[15] Cybyk B Z, Wilkerson J T, Grossman K R 2004 2nd AIAA Flow Control Conference Portland Oregon, USA, June 28-July 1, 2004
[16] Narayanaswamy V, Raja L L, Clemens N T 2012 AIAA J. 50 246
[17] Anderson K, Knight D D 2012 AIAA J. 50 1855
[18] Caruana D, Barricau P, Hardy P, Cambronne J P, Belinger A 2009 47th AIAA Aerospace Sciences Meeting Inculding the New Horizons Forum and Aerospace Exposition Orlando Florida, USA, January 5-8, 2009
[19] Belinger A, Hardy P, Gherardi N, Naudé N, Cambronne J P, Caruana D 2011 IEEE Trans. Plasma. Sci. 39 2334
[20] Belinger A, Hardy P, Barricau P, Cambronne J P, Caruana D 2011 J. Phys. D: Appl. Phys. 44 365201
[21] Shin J 2010 Chin. J. Aeronaut. 23 518
[22] Shan Y, Zhang J Z, Tan X M 2011 J. Aero. Power 26 551 (in Chinese) [单勇, 张靖周, 谭晓茗 2011 航空动力学报 26 551]
[23] Jia M, Liang H, Song H M, Liu P C, Wu Y 2011 High Voltage Engin. 37 1493 (in Chinese) [贾敏, 梁华, 宋慧敏, 刘朋冲, 吴云 2011 高电压技术 37 1493]
[24] Liu P C, Li J, Jia M, Wen B 2011 J. Air Force Eng. Univ. 12 22 (in Chinese) [刘朋冲, 李军, 贾敏, 文彬 2011 空军工程大学学报 12 22]
[25] Jayaraman B, Shyy W 2008 Prog. Aerospace Sci. 44 139
[26] Cheng Y F, Nie W S, Che X K 2012 Chin. Sci. Bull. 57 2164 (in Chinese) [程钰锋, 聂万胜, 车学科 2012 科学通报 57 2164]
[27] Zhang P F, Liu A B, Wang J J 2010 Sci. China Tech. Sci. 53 2772
[28] Ekici O, Ezekoye O A, Hall M J, Matthewa R D 2007 J. Fluid Eng. ASME. 129 55
[29] D'Angola A, Colonna G, Gorse G, Capitelli M 2008 Eur. Phys. J. D 46 129
[30] Naghizadeh-Kashani Y, Cressault Y, Gleizes A 2002 J. Phys. D: Appl. Phys. 35 2925
[31] Zhou Q H, Li H, Xu X, Liu F, Guo S F, Chang X J, Guo W K, Xu P 2009 J. Phys. D: Appl. Phys. 42 015210
[32] Akram M 1996 AIAA J. 34 1835
[33] Yang S M, Tao W Q 1998 Heat Transfer (Beijing: Higher Education Press) p5 (in Chinese) [杨世铭, 陶文铨 1998 传热学 (北京: 高等教育出版社) 第5页]
[34] Greason W D, Kucerovsky Z, Bulach S, Flatley M W 1997 IEEE Trans. Ind. Appl. 33 1519
[35] Wang L, Luo Z B, Xia Z X, Liu B, Deng X 2012 Sci. China Tech. Sci. 55 2225
[36] Narayanaswamy V 2010 Ph. D. Dissertation (Austin: the University of Texas at Austin)
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[1] Corke T C, Enloe C L, Wilkinson S P 2010 Annu. Rev. Fluid Mech. 42 505
[2] Leonov S, Yarantsev D 2008 J. Propul. Power 24 1168
[3] Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y 2009 J. Phys. D: Appl. Phys. 42 165503
[4] Grossman K R, Cybyk B Z, van Wie D M 2003 41st Aerospace Science Meeting and Exhibit Reno Nevada, USA, January 6-9, 2003
[5] Roth J 2003 Phys. Plasmas 42 165503
[6] Moreau E 2007 J. Phys. D: Appl. Phys. 40 605
[7] Zhang P F, Wang J J, Feng L H, Wang G B 2010 AIAA J. 48 249
[8] Li Y H, Wu Y, Liang H, Song H M, Jia M 2010 Chin. Sci. Bull. 55 3060 (in Chinese) [李应红, 吴云, 梁华, 宋慧敏, 贾敏 2010 科学通报 55 3060]
[9] Li G, Li Y M, Xu Y J, Zhang Y, Li H M, Nie C Q, Zhu J Q 2009 Acta Phys. Sin. 58 4026 (in Chinese) [李刚, 李轶明, 徐燕骥, 张翼, 李汉明, 聂超群, 朱俊强 2009 58 4026]
[10] Wang J, Li Y H, Cheng B Q, Su C B, Song H M, Wu Y 2009 Acta Phys. Sin. 58 55113 (in Chinese) [王健, 李应红, 程邦勤, 苏长兵, 宋慧敏, 吴云 2009 58 5513]
[11] Cheng Y F, Nie W S, Li G Q 2012 Acta Phys. Sin. 61 060510 (in Chinese) [程钰锋, 聂万胜, 李国强 2012 61 060510]
[12] Narayanaswamy V, Raia L L, Clemens N T 2010 AIAA J. 48 297
[13] Haack S, Taylor T, Emhoif J, Cybyk B 2010 5th Flow Control Conference Chicago Illinois, USA, June 28-July 1, 2010
[14] Ko H S, Haack S J, Land H B, Cybyk B, Katz J, Kim H J 2010 Flow Meas. Instrum. 21 443
[15] Cybyk B Z, Wilkerson J T, Grossman K R 2004 2nd AIAA Flow Control Conference Portland Oregon, USA, June 28-July 1, 2004
[16] Narayanaswamy V, Raja L L, Clemens N T 2012 AIAA J. 50 246
[17] Anderson K, Knight D D 2012 AIAA J. 50 1855
[18] Caruana D, Barricau P, Hardy P, Cambronne J P, Belinger A 2009 47th AIAA Aerospace Sciences Meeting Inculding the New Horizons Forum and Aerospace Exposition Orlando Florida, USA, January 5-8, 2009
[19] Belinger A, Hardy P, Gherardi N, Naudé N, Cambronne J P, Caruana D 2011 IEEE Trans. Plasma. Sci. 39 2334
[20] Belinger A, Hardy P, Barricau P, Cambronne J P, Caruana D 2011 J. Phys. D: Appl. Phys. 44 365201
[21] Shin J 2010 Chin. J. Aeronaut. 23 518
[22] Shan Y, Zhang J Z, Tan X M 2011 J. Aero. Power 26 551 (in Chinese) [单勇, 张靖周, 谭晓茗 2011 航空动力学报 26 551]
[23] Jia M, Liang H, Song H M, Liu P C, Wu Y 2011 High Voltage Engin. 37 1493 (in Chinese) [贾敏, 梁华, 宋慧敏, 刘朋冲, 吴云 2011 高电压技术 37 1493]
[24] Liu P C, Li J, Jia M, Wen B 2011 J. Air Force Eng. Univ. 12 22 (in Chinese) [刘朋冲, 李军, 贾敏, 文彬 2011 空军工程大学学报 12 22]
[25] Jayaraman B, Shyy W 2008 Prog. Aerospace Sci. 44 139
[26] Cheng Y F, Nie W S, Che X K 2012 Chin. Sci. Bull. 57 2164 (in Chinese) [程钰锋, 聂万胜, 车学科 2012 科学通报 57 2164]
[27] Zhang P F, Liu A B, Wang J J 2010 Sci. China Tech. Sci. 53 2772
[28] Ekici O, Ezekoye O A, Hall M J, Matthewa R D 2007 J. Fluid Eng. ASME. 129 55
[29] D'Angola A, Colonna G, Gorse G, Capitelli M 2008 Eur. Phys. J. D 46 129
[30] Naghizadeh-Kashani Y, Cressault Y, Gleizes A 2002 J. Phys. D: Appl. Phys. 35 2925
[31] Zhou Q H, Li H, Xu X, Liu F, Guo S F, Chang X J, Guo W K, Xu P 2009 J. Phys. D: Appl. Phys. 42 015210
[32] Akram M 1996 AIAA J. 34 1835
[33] Yang S M, Tao W Q 1998 Heat Transfer (Beijing: Higher Education Press) p5 (in Chinese) [杨世铭, 陶文铨 1998 传热学 (北京: 高等教育出版社) 第5页]
[34] Greason W D, Kucerovsky Z, Bulach S, Flatley M W 1997 IEEE Trans. Ind. Appl. 33 1519
[35] Wang L, Luo Z B, Xia Z X, Liu B, Deng X 2012 Sci. China Tech. Sci. 55 2225
[36] Narayanaswamy V 2010 Ph. D. Dissertation (Austin: the University of Texas at Austin)
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